View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45358U 26144.76142433 +.00000000 +00000-0 +00000-0 0 00005
2 45358 64.3701 313.2419 0007534 232.9765 126.9500 2.13102336 08
| Epoch (UTC): | 24 May 2026 18:16:27 |
| Eccentricity: | 0.0007534 |
| inclination: | 64.3701° |
| perigee height: | 19111 km |
| apogee height: | 19149 km |
| right ascension of ascending node: | 313.2419° |
| argument of perigee: | 232.9765° |
| revolutions per day: | 2.13102336 |
| mean anomaly at epoch: | 126.9500° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|